FIELD: heating.
SUBSTANCE: group of inventions relates to equipment of pre-launch activities of space vehicle. Device includes counterflow regenerative liquid-liquid heat exchanger included in the heating medium circulation circuit of the space vehicle thermal control. This device is connected with ground device of thermal conditioning by means of the quick-release coolant supply and removal pipelines with quick-release connections. In this device quick-release pipelines and quick-release connections are provided with thermal insulation. Under the first option quick-release connections are installed of the space vehicle at right angle to the plane passing through the longitudinal axis of the payload fairing having hatch for quick-release connection. Under the second option the quick-release connection is installed on the space vehicle parallel to the longitudinal axis of the payload fairing, and another part of the quick-release connection connected with the first by means of the quick-release pipeline is installed on the adapter section with the appropriate hatch.
EFFECT: increased efficiency of thermal conditioning of space vehicle onboard equipment at high heat generation and wide range of ambient temperatures.
2 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR TEMPERATURE CONTROL OF ON-BOARD EQUIPMENT OF THE PAYLOAD WITHIN THE SPACE NOSE CONE | 2017 |
|
RU2661270C1 |
| SPACE OBJECT TEMPERATURE CONTROL SYSTEM | 2002 |
|
RU2216490C1 |
| METHOD FOR TEMPERATURE CONTROL OF ONBOARD EQUIPMENT OF PAYLOAD LOCATED INSIDE HEAD FAIRING OF SPACE HEAD PART OF SPACE ROCKET, AND DEVICE FOR ITS IMPLEMENTATION | 2017 |
|
RU2673439C1 |
| SPACE CENTER COMPLEX FOR PREPARATION OF CARRIER ROCKET WITH ASCENT UNIT EQUIPPED WITH SUSTAINER, AND SPACESHIP | 2011 |
|
RU2480389C2 |
| SPACE VEHICLE LAUNCHING SITE COMPLEX FOR ROCKER CARRIER PREPARATION FOR LAUNCHING | 2011 |
|
RU2479472C2 |
| LAUNCHING COMPLEX FOR PRE-LAUNCH PREPARATION AND LAUNCHING OF LAUNCH VEHICLE WITH SPACE NOSE CONE (VERSIONS) | 2006 |
|
RU2318706C1 |
| DEVICE TO CONTROL THERMAL CONDITIONS AND CLEANLINESS OF SPACECRAFT HEAD WITH LARGE-SIZED PAYLOAD | 2014 |
|
RU2557092C1 |
| AEROSTATIC ROCKET AND SPACE COMPLEX | 2017 |
|
RU2682893C1 |
| METHOD TO PROVIDE THERMAL CONDITIONS AND CLEANLINESS OF ENVIRONMENT FOR PAYLOAD UNDER ASSEMBLY-PROTECTION UNIT OF SPACE-MISSION MISSILE AND DEVICES FOR ITS IMPLEMENTATION (VERSIONS) | 2013 |
|
RU2543441C1 |
| METHOD FOR MAINTENANCE OF THERMAL RATE OF ONBOARD DEVICES IN COMPARTMENT OF SPACE LAUNCH VEHICLES | 2018 |
|
RU2678731C1 |
